ES2596555T3 - Estructura de aeronave con medios de reducción del riesgo de desprendimiento en áreas de deformación diferente - Google Patents
Estructura de aeronave con medios de reducción del riesgo de desprendimiento en áreas de deformación diferente Download PDFInfo
- Publication number
- ES2596555T3 ES2596555T3 ES12834607.9T ES12834607T ES2596555T3 ES 2596555 T3 ES2596555 T3 ES 2596555T3 ES 12834607 T ES12834607 T ES 12834607T ES 2596555 T3 ES2596555 T3 ES 2596555T3
- Authority
- ES
- Spain
- Prior art keywords
- structural member
- stringer
- interface component
- flexible interface
- liner
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 230000009975 flexible effect Effects 0.000 claims abstract description 59
- 239000000853 adhesive Substances 0.000 claims abstract description 27
- 230000001070 adhesive effect Effects 0.000 claims abstract description 27
- 229920001971 elastomer Polymers 0.000 claims abstract description 12
- 229920001973 fluoroelastomer Polymers 0.000 claims abstract description 3
- 238000000034 method Methods 0.000 claims description 17
- 229920000459 Nitrile rubber Polymers 0.000 claims description 4
- 239000003365 glass fiber Substances 0.000 claims description 3
- 239000012779 reinforcing material Substances 0.000 claims 2
- 239000000463 material Substances 0.000 description 21
- 239000002131 composite material Substances 0.000 description 9
- 238000004519 manufacturing process Methods 0.000 description 7
- 230000032798 delamination Effects 0.000 description 6
- 238000004026 adhesive bonding Methods 0.000 description 5
- 238000004513 sizing Methods 0.000 description 5
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 4
- 238000005304 joining Methods 0.000 description 4
- 239000010936 titanium Substances 0.000 description 4
- 229910052719 titanium Inorganic materials 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 239000011152 fibreglass Substances 0.000 description 3
- 238000005253 cladding Methods 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 239000003292 glue Substances 0.000 description 2
- 239000007769 metal material Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 229920002449 FKM Polymers 0.000 description 1
- 239000004677 Nylon Substances 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 239000004918 carbon fiber reinforced polymer Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B3/00—General-purpose turning-machines or devices, e.g. centre lathes with feed rod and lead screw; Sets of turning-machines
- B23B3/08—Turning-machines characterised by the use of faceplates
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B25/00—Layered products comprising a layer of natural or synthetic rubber
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B25/00—Layered products comprising a layer of natural or synthetic rubber
- B32B25/02—Layered products comprising a layer of natural or synthetic rubber with fibres or particles being present as additives in the layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
- B32B3/08—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions characterised by added members at particular parts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/064—Stringers; Longerons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/20—Integral or sandwich constructions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/101—Glass fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31855—Of addition polymer from unsaturated monomers
- Y10T428/31931—Polyene monomer-containing
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Laminated Bodies (AREA)
- Adhesives Or Adhesive Processes (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/291,667 US8985516B2 (en) | 2011-11-08 | 2011-11-08 | Reducing risk of disbonding in areas of differing strain |
| US201113291667 | 2011-11-08 | ||
| PCT/US2012/052726 WO2013074174A2 (en) | 2011-11-08 | 2012-08-28 | Reducing risk of disbonding in areas of differing strain |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2596555T3 true ES2596555T3 (es) | 2017-01-10 |
Family
ID=47997767
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES12834607.9T Active ES2596555T3 (es) | 2011-11-08 | 2012-08-28 | Estructura de aeronave con medios de reducción del riesgo de desprendimiento en áreas de deformación diferente |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US8985516B2 (de) |
| EP (1) | EP2776314B1 (de) |
| ES (1) | ES2596555T3 (de) |
| WO (1) | WO2013074174A2 (de) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10479475B2 (en) * | 2013-08-09 | 2019-11-19 | The Boeing Company | Composite stringer beam joint structure of an aircraft |
| DE102016210076B3 (de) * | 2016-06-08 | 2017-08-10 | Ford Global Technologies, Llc | Fahrzeugkomponente mit einem Anbindungsbereich zur elastischen Anbindung einer anderen Komponente |
| DE102016210077A1 (de) | 2016-06-08 | 2017-12-14 | Ford Global Technologies, Llc | Fahrzeugkomponente mit einem Anbindungsbereich zur elastischen Anbindung einer anderen Komponente |
| DE202016103195U1 (de) | 2016-06-08 | 2016-07-08 | Ford Global Technologies, Llc | Fahrzeugkomponente mit einem Anbindungsbereich zur elastischen Anbindung einer anderen Komponente |
| US10677090B2 (en) * | 2017-05-10 | 2020-06-09 | General Electric Company | Component having co-bonded composite and metal rings and method of assembling same |
| ES2906760T3 (es) * | 2019-02-19 | 2022-04-20 | Muelles Y Ballestas Hispano Alemanas Projects S L | Panel rigidizado en materiales compuestos y procedimiento de fabricación de dicho panel |
| GB2587391A (en) * | 2019-09-26 | 2021-03-31 | Airbus Operations Ltd | Aircraft assembly |
| KR20240148479A (ko) * | 2023-04-04 | 2024-10-11 | 현대자동차주식회사 | 동체의 날개 하중 지지구조 |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2304718A (en) * | 1940-07-15 | 1942-12-08 | Gen Tire & Rubber Co | Structural member and method of fabricating the same |
| US4113910A (en) | 1977-04-27 | 1978-09-12 | Rockwell International Corporation | Composite load coupler for reinforcing composite structural joints |
| US4574986A (en) * | 1983-02-18 | 1986-03-11 | Aero Tec Laboratories, Inc. | Flexible container system |
| US5240759A (en) * | 1989-12-04 | 1993-08-31 | Layton Charles B | Aircraft fuel mat |
| US6386481B1 (en) * | 2001-01-08 | 2002-05-14 | Patria Finavicomp Oy | Arrangement for fastening stringers to aircraft wing ribs |
| US8444087B2 (en) | 2005-04-28 | 2013-05-21 | The Boeing Company | Composite skin and stringer structure and method for forming the same |
| US7611595B2 (en) | 2006-02-01 | 2009-11-03 | Lockheed Martin Corporation | System, method, and apparatus for metallic-composite joint with compliant, non-corrosive interface |
| US20080245929A1 (en) * | 2006-10-06 | 2008-10-09 | The Boeing Company | Systems and Methods for Fabricating Multi-Material Joining Mechanisms |
| US7997534B2 (en) * | 2006-10-13 | 2011-08-16 | Airbus Operations Gmbh | Connecting structure for an aircraft or spacecraft and method for producing the same |
| DE102006048641B4 (de) | 2006-10-13 | 2015-04-16 | Airbus Operations Gmbh | Verbindungsstruktur für ein Luft- oder Raumfahrzeug und Verfahren zum Herstellen derselben |
| DE102009060693A1 (de) | 2009-12-29 | 2011-06-30 | Airbus Operations GmbH, 21129 | Versteifungselement für ein Luftfahrzeug und Flächengebilde mit einem derartigen Versteifungselement |
-
2011
- 2011-11-08 US US13/291,667 patent/US8985516B2/en active Active
-
2012
- 2012-08-28 EP EP12834607.9A patent/EP2776314B1/de active Active
- 2012-08-28 WO PCT/US2012/052726 patent/WO2013074174A2/en not_active Ceased
- 2012-08-28 ES ES12834607.9T patent/ES2596555T3/es active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US8985516B2 (en) | 2015-03-24 |
| WO2013074174A3 (en) | 2013-07-18 |
| EP2776314A2 (de) | 2014-09-17 |
| EP2776314B1 (de) | 2016-08-10 |
| WO2013074174A2 (en) | 2013-05-23 |
| US20130112812A1 (en) | 2013-05-09 |
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